Integrated control algorithm based on solid propellant micro-thruster array

Xu Hui Liu*, Shu Zhou Fang, Hong Peng Ma, Qing Feng Gao

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

In order to make solid propellant micro-thruster array more practical, the layout method which can be used in attitude and orbit control was proposed. The mathematical model of allocation algorithm was established and the concept was introduced to ensure that the least thrusters were used. The dynamic programming and the greedy strategy were introduced into the problem and the solving mathematical model was established. Through analysis and simulation, this method can effectively solve the problem, which is conductive to achieve real-time control.

Original languageEnglish
Pages (from-to)17-23
Number of pages7
JournalGuti Huojian Jishu/Journal of Solid Rocket Technology
Volume35
Issue number1
Publication statusPublished - Feb 2012

Keywords

  • Allocation algorithm
  • Array programming algorithm
  • Real-time control
  • Solid propellant micro-thruster array
  • Thrusters layout

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